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| |
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| Engine make/model: | Lycoming O-540-B4B5
|
| Horsepower@altitude: | 235@SL |
| Horsepower for takeoff: | 235 |
TBO hrs.:
| 2000 |
| Fuel type: | 100/100LL
|
Propeller type/diameter:
| Hartzell CS
|
Landing gear type:
| Tri/Fixed
|
| Max ramp weight (lbs.): | 3000
|
| Gross weight (lbs.): | 3000 |
| Landing weight (lbs.): | 3000
|
| Empty weight, std. (lbs.): | 1550
|
| Useful load, std. (lbs.): | 1450
|
Payload, full std. fuel (lbs.):
| 958
|
| Usable fuel (gals.): | 82 |
| Oil capacity (qts.): | 12
|
| Wingspan: | 32 ft. |
| Overall length: | 24 ft. |
| Height: | 7 ft. 10 in. |
| Wing area (sq. ft.): | 170 |
Wing loading (lbs./sq. ft.):
| 17.6
|
Power loading (lbs./hp.):
| 12.8 |
Wheel size (in.):
| 6.00 x 6
|
| Seating capacity: | 4
|
Cabin doors:
| 1
|
| Cabin width (in.): | 44 |
| Cabin height (in.): | 47 |
| Baggage capacity (lbs.): | 200
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| |
PERFORMANCE |
| Cruise speed (kts.): | |
| 75% power: | 133 |
| 65% power: | 127* |
55% power:
| 122* |
| | |
| Max range (w/ reserve) (nm): | |
75% power:
| 718** |
65% power:
| 813**
|
55% power:
| 939**
|
| | |
Fuel consumption (gph):
| |
| 75% power: | 12.8** |
| 65% power: | 11.1** |
55% power:
| 9.4** |
| | |
| Estimated endurance (65%) (hrs): | 6.4**
|
Vs (kts.):
| 57
|
Vso (kts.):
| 52
|
| Best rate of climb (SL fpm): | 800 |
Best rate of climb, 8000 ft. (fpm):
| 400*
|
| Service ceiling (ft.): | 13,550 |
| Takeoff ground roll (ft.): | 850 |
| Takeoff over 50-ft. obstacle (ft.): | 1410
|
| Landing ground roll (ft.): | 1040 |
Landing over 50-ft. obstacle (ft.):
| 1740
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| |
*estimated
|
| **calculated |
Sources: Aircraft Bluebook Price Digest, Jane’s All The World’s Aircraft
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